Advanced Aeromarine Carrera

Last updated
Carrera
Role Homebuilt ultralight aircraft
First flight 1990s
Variants Arnet Pereyra Sabre II

The Carrera is a two-seat ultralight aircraft marketed for home building. Designed by Advanced Aeromarine, it has also been marketed by Advanced Aviation and Arnet Pereyra Inc. It is a high-wing taildragger aircraft of pusher configuration with side-by-side seating. It is of fabric-covered tubular construction.

Ultralight aviation aviation field involving design, regulation, and operation of very lightweight aircraft

Ultralight aviation is the flying of lightweight, 1- or 2-seat fixed-wing aircraft. Some countries differentiate between weight-shift control and conventional 3-axis control aircraft with ailerons, elevator and rudder, calling the former "microlight" and the latter "ultralight".

Homebuilt aircraft planes constructed by persons for whom this is not a professional activity

Homebuilt aircraft, also known as amateur-built aircraft or kit planes, are constructed by persons for whom this is not a professional activity. These aircraft may be constructed from "scratch," from plans, or from assembly kits.

Advanced Aeromarine

Advanced Aeromarine was an aircraft manufacturer based in Ocoee, Florida. It built light aircraft and sailplanes, developing a number of successful designs that have been produced by a number of different firms over the years.

Contents

The aircraft was later marketed by Keuthan Aircraft as the Sabre and developed into the two-place Sabre II. [1]

Keuthan Aircraft was a US aircraft manufacturer located in Merritt Island, Florida. The firm marketed ultralights in kit form. It ceased business in 1996 and its assets were acquired by Arnet Pereyra Inc.

The Arnet Pereyra Sabre II is an American, two-seats in side-by-side configuration, conventional landing gear-equipped, strut-braced, high-wing ultralight trainer that was produced by Arnet Pereyra Inc of Rockledge, Florida in kit form for amateur construction.

Specifications (Carrera 180)

Data from [2]

General characteristics

Rotax 582 two-stroke piston aircraft engine

The Rotax 582 is a 48 kW (64 hp) two-stroke, two-cylinder, rotary intake valve, oil-in-fuel or oil injection pump, liquid-cooled, gear reduction-drive aircraft engine manufactured by BRP-Rotax GmbH & Co. KG. It is for use in non-certified aircraft operating in day visual flight rules.

Performance

  • Maximum speed: 75 mph (121 km/h; 65 kn)
  • Cruise speed: 63 mph (101 km/h; 55 kn)
  • Stall speed: 31 mph (50 km/h; 27 kn)
  • Service ceiling: 12,000 ft (3,700 m)
  • Rate of climb: 650 ft/min (3.3 m/s)

See also

Related development

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References

  1. ↑ Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page E-32. Cybair Limited Publishing, 2001. ISBN   0-9680628-1-4
  2. ↑ Terpstra, 1992, p.17.


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